N464WN
Service difficulty reports · 318
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N464WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N464WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2026092253284Comms Unit · malfunctionedLOSS OF COMMS 1/2 AND ACARS, FLYING THROUGH WEATHER. PERFORMED STATIC DISCHARGER INSPECTION IAW AMM 23-61-00, NO DEFECTS NOTED. PERFORMED VHF COMMS SYSTEM OPS CHK IAW AMM 23-12-00 NO DEFECTS NOTED. ACFT OK FOR SERVICE.SDR SWAA2026071420043Isolator · crackedFWD SERVICE DOOR ESCAPE SLIDE AFT ISOLATOR CRACKED. R & R FWD SERVICE DOOR ESCAPE SLIDE AFT ISOLATOR IAW SRM 51-40-02.SDR SWAA2026071320046Battery Pack · failedAFT RT EMERGENCY BATTERY PACK M1672 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.SDR SWAA2026071320045Battery Pack · failedAFT LEFT EMERGENCY BATTERY PACK M1673 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06SDR SWAA2026041383872Strap · crackedFOUND CRACK ON LEFT HAND WING LEADING EDGE TO WING LWR ATTACHMENT AT 452.75 WING STATION<[01] UPON FURTHER INVESTIGATION NO CRACK WAS FOUND. DAMAGE FOUND TO BE CORROSION ONLY. ALL CORROSION MAINTENANCE WILL BE ACCOMPLISHED ON FAULT TTG8Q01B6MKV;[02] VERIFIED: SDR SWAA2026040982147Scuff Plate · crackedFWD CARGO FWD CORNER SCUFF PLATE CRACKED<[01] LOCATED AND DRILLED REPLACEMENT FWD CARGO FWD CORNER SCUFF PLATE P/N 654A0004-337 LOT# 7530406 IAW SRM 51-40-05-0G-0 AND BOEING DWG# 143A8330 REV:-;[02] FWD CARGO; FWD CORNER SCUFF PLATE WILL BE INSTALLED ON TTG8Q0SDR SWAA2026040982251Scuff Plate · crackedAFT CARGO FWD CORNER SCUFF PLATE CRACKED<[01] LOCATED AND DRILLED AFT CARGO FWD CORNER SCUFF PLATE IAW B737 SRM 51-40-05-0G AND DRAWING 146A8340 REV - SCUFF PLATE TO BE INSTALLED ON FAULT TTG8Q01B8N46;[02] VERIFIED: LOCATED AND DRILLED AFT CARGO FWD CORNER SCUSDR SWAA2026040982252Web · corrodedCORROSION ALONG FWD CARGO DOOR TRHESHHOLD<[01] REMOVED AND REPLACED FWD CARGO THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND BOEING DWG# 143A8330 REV:-;[02] VERIFIED COMPLETE.SDR SWAA2026040982253Threshold · corrodedCORROSION ALONG AFT CARGO DOOR TRHESHOLD<[01] REMOVED AND REPLACED TRHESHOLD ON FWD CARGO; IAW B737 SRM 51-40-02-0G STEP 5; AND DWG 146A8340 R -;[02] CORRECTION TO CORRECTIVE ACTION: REMOVED AND REPLACED THRESHOLD ON AFT CARGO; IAW B737 SRM 51-40-02-0G STEP 5;SDR SWAA2026040980898Strap · crackedFOUND CRACK AND CORROSION ON LEFT HAND WING LEADING EDGE TO WING LWR ATTACHMENT AT 452.75 WING STATION.<[01] REPAIRED LEFT HAND WING LEADING EDGE TO WING LWR ATTACH STRAP AT WSTA 452.75 (OSS 227.95) PER EA 26-157-00825 TTG8Q01BKAXB;[02] VERIFIED: REPAIRED LEFTSDR SWAA2026022473875Quick Disconnect · leakingBRAKE SEVERELY SHUDDERING WHEN ATTEMPTING TO STOP AT THE GATE. COMING TO A STOP WAS VERY DIFFICULT. R & R NR 4 MLG BRAKE IAW AMM 32-41-41, FOUND NR 4 MLG BRAKE DISCONNECT TO BE LEAKING. R & R BRAKE DISCONNECT IAW AMM 32-42-11, PERFORMED BRAKE BLEEDING IAW AMSDR SWAA2026012864353Valve · failedHYDRAULIC B SYSTEM FAILURE. IF IT IS A PRIORITY VALVE THERE IS A DEVIATION ALL EA FOR THE CHECK OUT M-25-127-00862. R & R T/E FLAP FLOW LIMITER VALVE IAW AMM 27-51-67. OPS CHECKED. NO LEAKS DETECTED.SDR SWAA2025010682785Lamp · inoperativeEMERGENCY EXIT LIGHT - ABOVE F/O SIDE - EMERGENCY EXIT OUT<[01] RELAMPED F/O SIDE EMERGENCY EXIT LIGHT REF AMM 33-51-01. OPS CHK GOOD.SDR SWAA2024091135054Tail Cone · delaminatedFUSELAGE SECTION 48 DELAMINATION COMMON TO TAIL CONE<[01] PERFORMED PERMANENT REPAIR OF THE TAIL CONE IAW SRM 51-70-04SDR SWAA2024080722685Lens · brokenFO SIDE EMERGENCY EXIT LENS INDICATOR BROKEN<[01] REMOVE AND REPLACE FO SIDE EXIT LENS INDICATOR PER AMM 33-51-01. OPS CHECK GOOD.SDR SWAA2024062404772Slide · out of positionL2 DOOR SLIDE CATCHES ON THRESHOLD<[01] CORRECTED THE Z-FOLD ON L2 DOOR SLIDE AND TUCKED EXCESS GIRT MATERIAL IN REF WORK INSTRUCTIONS 725-61-06;[02] VERIFIED STEP 1.SDR SWAA2024062401925Sign · brokenAFT LOWERED CEILING PANEL EXIT SIGN BROKEN<[01] REMOVED AND REPLACED AFT CEILING PANEL EXIT SIGN ASSEMBLY AS PER B737 AMM 33-51-01-960-802. OPS CHECK PASSED.;[02] VERIFIED STEP 1.SDR SWAA2024062599500Light · glazedMAIN CABIN PHOTOLUMINESCENT ARE GLAZED/SCRATCHED<[01] REMOVED AND REPLACED MAIN CABIN PHOTOLUMINESCENT IN REF AMM-33-51-15-000-802; 33-51-15-400-802;[02] CORRECTION: REMOVED AND REPLACED MAIN CABIN PHOTOLUMINESCENT IN REF AMM-33-51-15-000-802; 33-51-15-400-802SDR SWAA2024062597847Battery Pack · no testSEVERAL PAX CABIN EMERGENCY LIGHT BATTERIES WILL NOT HOLD CHARGE<[01] REMOVED AND REPLACED PAX EMERGENCY LIGHT BATTERY PACK M1675 I/A/W BOEING AMM 33-51-06-960-805; OPS CHECK NORMAL;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02SDR SWAA2024062691159Skin · delaminatedL/WING O/B AFT FLAP I/B LOWER T/EDGE SKIN AREA DELAMINATED FOUND OUT-LIMIT<[01] REMOVED & INSTALLED LEFT WING O/B AFT FLAP AS PER AMM 27-51-22-400-801. ACCOMPLISHED ADJUSTMENT FOUND TO BE WITHIN LIMITS. <BR>DIGITAL CALIPER USED BC 175307 DUE DATE 05-DEC-24<BR>SDR SWAA2024062590273Seal · crackedR/H HOR. STAB FWD UPPER SLIDER SEAL CRACKED.<[01] REMOVED STABILIZER TO BODY UPPER FRONT SPAR SLIDING SEAL AS PER AMM 53-31-31-000-802; TRANSFERED TIE-BAR AND CORNER PLATES FROM OLD SEAL PLATE TO NEW SEAL PLATE REF SRM 51-40-02-0G-0; AND INSTALLED STABILIZER TSDR SWAA2024062589194Plate · damagedLH WING DEFLECTOR RIB ATTACH SERRATED PLATE HOLES ELONGATED<[01] REMOVED BOLTS AT L/H WING DEFLECTOR CONTROL RIB UPPER TAB IN REF B737-700 SRM 51-40-02-0G-0; AFTER FURTHER INSPECTION FOUND NO ENLONGATED HOLES; AND NO SERRATED PLATES DAMAGE; REPLACED BOLTS IN RSDR SWAA2024062589195Bracket · damagedRIGHT WING TRAILING EDGE ACCESS PANEL 651GB ROD CONNECTED TO I/B AFT BRACKET UPPER BRACKET HOLE ELONGATED<[01] REMOVED AND INSTALLED NEW BRACKET AT PANEL # 651GB RIGHT WING TRAILING EDGE AS PER SRM 51-40-02-0G-0 AND AIPC 57-15-00-09.;[02] VERIFIED CORRECTIVE ASDR SWAA2024062589199Bracket · damagedRIGHT WING TRAILING EDGE ACCESS PANEL 651GB I/B AFT BRACKET HOLE ELONGATED<[01] REMOVED AND INSTALLED NEW BRACKET AT PANEL # 651GB RIGHT WING TRAILING EDGE AS PER SRM 51-40-02-0G-0 AND AIPC 57-15-00-09.;[02] VERIFIED CORRECTIVE ACTION STEP 1<BR><BR>AUDIT C/W RSDR SWAA2024062589196Bracket · corrodedEVIDENCE OF CORROSION UNDER SEALANT AT LEFT AFT BOOST PUMP BONDING STRAP<[01] REMOVED AND REPLACED BOTH UPPER AND LOWER BONDING STRAPS/BRACKETS AT LEFT WING AFT BOOST PUMP IAW SRM 51-40-02-0G-0; AIPC 28-22-41-05; AMM 20-10-44-400-801. PERFORMED ELECTRICAL RESISDR SWAA2024062401200Access Panel · damagedRIGHT WING TRAILING EDGE ACCESS PANEL 651GB SECOND BRACKET FROM I/B ROD HOLE ELONGATED<[01] REMOVED AND INSTALLED NEW BRACKET AT PANEL # 651GB RIGHT WING TRAILING EDGE AS PER SRM 51-40-02-0G-0 AND AIPC 57-15-00-09.;[02] VERIFIED CORRECTIVE ACTION STEP 1<BR><BRSDR SWAA2024062489490Scuff Plate · crackedFOUND FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE CRACKED<[01] SCUFFPLATE WAS REPAIRED BY OUTSIDE VENDOR PO #414715 INSTALLATION OF SCUFFPLATE WILL BE ACCOMPLISHED ON CARD TTG8Q001TFBY;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02SDR SWAA2024062489201Door Frame · crackedFORWARD GALLEY SERVICE DOOR (R-1) CUTOUT UPPER FWD CORNER FRAME CRACK<[01] REMOVED AND REPLACED FORWARD GALLEY SERVICE DOOR (R-1) CUTOUT UPPER FWD CORNER FRAME REF SRM 51-40-02-0G-0 AND DWG 141A8370;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02SDR SWAA2024062588997Intercostal · corrodedE&E COMP CORROSION ON INTERCOSTAL BS 344-360 S23L. PARTIALLY INSTALLED INTERCOSTAL IAW SRM 51-40-02 & DWG 141A8131. REMOVED AND REPLACED INTERCOSTAL BS 344-360, S23L IAW 51-40-02, & DWG 141A8131. APPLIED EWIS PROTECTION AS REQUIRED IAW AMM 20-60-07-913-80SDR SWAA2024062488998Intercostal · crackedCRACK INDICATION OBTAINED FROM FWD FASTENER HOLE OF INTERCOSTAL AT COCKPIT FLOOR STA 250 RBL 4.<[01] ACCOMPLISHED EA 24-153-01485. REF FAULT TTG8Q00TH8E7;[02] STEP 1 IN CORRECTIVE ACTION ENTER IN ERROR;[03] ACCOMPLISHED EA 24-153-01485;[04] VERIFIED STEP 3SDR SWAA2024062588645Floor Support · crackedMAIN CABIN WING CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT STA 540 LBL 1 MKD DOT<[01] REMOVED AND REPLACED FLOOR SUPPORT BRACKET AT MAIN CABIN STA 540 LBL 1' AS PER SRM 51-40-02-0G-0 AND DWG 143A0060.;[02] VERIFIED STEP 1.;[03] AUDIT C/W PER MPM 52.02.02.SDR SWAA2024062588641Floorbeam · crackedMAIN CABIN WING CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT STA 540 RBL 1. FAULT RESOLVED ON OTHER FAULT. WORK ACCOMPLISHED ON TTG8Q00TE4QN.;[02] VERIFIED STEP 1.<BR>AUDIT C/W PER MPM 52.02.02.SDR SWAA2024062588642Floor Panel · crackedMAIN CABIN WING CENTER SECTION FLOOR PANEL 231YF CRACKED AT AFT END MKD DOT<[01] PERFORMED DRY OUT; PREPARED DAMAGE AREA AND APPLIED PERMANENT REPAIR ON PANEL#231YF AS PER B737 SRM 53-00-50-2R-7 MATERIAL USED PO#1690453 PO#2039827;[02] CORRECTION TO STEP 1: PESDR SWAA2024062588647Floor Support · corrodedMAIN CABIN WING CENTER SECTION FLOOR SUPPORT INNER CHORD CORRODED FROM STA 639-5' TO STA 639+8' RBL 64 . REMOVED AND REPLACED FLOOR SUPPORT INNER CHORD AT STA 639 -5 TO 639 +8 RBL 64 IN MAIN CABIN CENTER SECTION IAW SRM 51-40-02-0G-0 AND DWG 144A5901.SDR SWAA2024062488644Skin · crackedL/H WING I/B AFT FLAP LOWER SURFACE SKIN CRACK AT 28.25' O/B EDGE & 5' T/E<[01] NSTALLED REPAIR AT L/H WING I/B AFT FLAP ON LOWER SURFACE SIZE OF REPAIR 3' DIAMETER PER B737SRM 51-70-10-2R-0 PARAGRAPH(20.B) MATERIAL USED ADHESIVE AF163-2K-06 PO#2053056 AND TOOSDR SWAA2024062587816Gusset · crackedFWD CARGO COMP STA 500D STR 19L GUSSET CRACKED. REMOVED AND REPLACED GUSSET AT FWD CARGO COMP STA 500D STR 19L AS PER SRM 51-40-02-0G-0 & 143A7902.SDR SWAA2024062587817Gusset · crackedFWD CARGO COMP STA 500D STR 19R GUSSET CRACK. REMOVED AND REPLACED GUSSET AT FWD CARGO COMP STA 500D STR 19R AS PER SRM 51-40-02-0G-0 & DWG 143A9481.SDR SWAA2024062587670Stringer · corrodedAREA AFT OF FWD CARGO STA 540 STR 26L LOWER SECTION CORROSION. ACOMPLISHED REPAIR ON STR 26L AFT OF FWD CARGO STA 540 AS PER SRM 51-40-02-0G-0 AND EA 24-153-01393.SDR SWAA2024062587678Skin · delaminatedL/W OUB AFT FLAP INB LOWER T/E I/B TIP SKIN AREA DELAMINATED MKD DOT<[01] FLAP IS BEEING REPLACED ON WORK CARD TTG8Q00TMGD9;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02SDR SWAA2024062487687Web · crackedAFT CARGO DOOR CUTOUT LOWER WEB CRACK AT STA 807+2'<[01] REMOVED AND REPLACED WEB AT AFT CARGO DOOR CUTOUT SRM 51-40-02-0G-0 AND DWG 146A8123;[02] VERIFIED STEP 1<BR>AUDIT C/W AS PER 52.02.02SDR SWAA2024062587264Panel · peelingPANEL 431DL INNER SURFACE IS PEELING<[01] REPAIRED INNER SURFACE PANEL 431DL. AS PER; SRM 51-70-14-2R-3.;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02SDR SWAA2024062487276Scuff Plate · crackedFOUND AFT CARGO AFT CORNER SCUFF PLATE CRACKED<[01] AFT CARGO AFT CORNER WAS REPAIRED BY OUTSIDE VENDOR JL WELDING UNDER PO # 414704 USING GUIDELINES ON REFERENCE SRM 53-60-15-2R-1 REPAIR 1. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q001TFAV;[02] VERISDR SWAA2024062587249Floor Panel · frayedMAIN CABIN FLOOR PANEL 221BF UPPER SURFACE FRAYING<[01] REMOVED AND INSTALLED MAIN CABIN FWD WET AREA FLOOR PANEL 221BF IN REF 53-21-00-000-801; 53-21-00-400-801;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02SDR SWAA2024062587252Floor Panel · frayedMAIN CABIN FLOOR PANEL 222BF UPPER SURFACE FRAYING<[01] REMOVED AND INSTALLED MAIN CABIN FWD WET AREA FLOOR PANELS 222BF IN REF AMM-53-21-00-000-801; 53-21-00-400-801;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02SDR SWAA2024062587253Floor Panel · frayedMAIN CABIN FLOOR PANEL 242VF UPPER SURFACE FRAYING<[01] REMOVED AND INSTALLED MAIN CABIN FLOOR PANEL 242VF AS PER AMM-53-21-00-000-801 AND AMM 53-21-00-400-801;[02] VERIFIED STEP 1. <BR><BR>AUDIT C/W AS PER MPM 52.02.02SDR SWAA2024062587250Stringer · crackedAREA AFT OF FWD CARGO STA 540 STR 23R LOWER SECTION CRACK<[01] ACCOMPLISHED REPAIR PER EA 24-153-01392 AND SRM 53-00-03-2R-1;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02SDR SWAA2024062587251Stringer · crackedAREA AFT OF FWD CARGO STA 540 STR 23L LOWER SECTION CRACK<[01] THIS REPAIR WAS ACCOMPLISHED ON TASK CARDS TTG8Q00TML8P- 24-153-01394-WIP1; TTG8Q00TSFFY- 24-153-10394-WIP2; TTG8Q00TT1F1- 24-153-01394-WIP3 AND TTG8Q00TVJFV- 24-153-01394- WIP 4. STRINGER 23L REPASDR SWAA2024062587256Angle · crackedMAIN CABIN STA 540 RBL 1' PANEL BREAK ANGLE CRACK<[01] REMOVED AND REPLACED PANEL ANGLE AT MAIN CABIN STA 540 RBL 1' AS PER SRM 51-40-02-0G-0 AND DWG 143A0060.;[02] VERIFIED STEP 1.<BR>AUDIT C/W PER MPM 52.02.02.SDR SWAA2024062587258Rib · crackedLH HORIZONTAL STABILIZER L/E PANEL 331B #3 RIB CRACK COUNTING FROM I/B TO O/B<[01] REMOVED AND REPLACED NEW RIB#3 AT LH HORIZONTAL STABILIZER L/E PANEL 331B REF 51-40-02-0G-0;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02SDR SWAA2024062587260Rib · crackedLH HORIZONTAL STABILIZER L/E PANEL 331B #4 RIB CRACK COUNTING FROM I/B TO O/B<[01] REMOVED AND REPLACED NEW RIB#4 AT LH HORIZONTAL STABILIZER L/E PANEL 331B REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02
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